Difference between revisions of "Atlas V"

From Marspedia
Jump to: navigation, search
(New page: thumb|200px|right|The '''Atlas V''' Rocket launches the [[Mars Reconnaissance Orbiter into space.]] The '''Atlas V''' rocket is an expendable launch vehicle forme...)
 
 
(11 intermediate revisions by 5 users not shown)
Line 1: Line 1:
[[Image:MRO_Launch.jpg|thumb|200px|right|The '''Atlas V''' Rocket launches the [[Mars Reconnaissance Orbiter]] into space.]]
+
[[Image:MRO_Liftoff.jpg|thumb|200px|right|The '''Atlas V''' Rocket launches the [[Mars Reconnaissance Orbiter]] into space.]]
  
The '''Atlas V''' rocket is an expendable launch vehicle formerly built by the [[Lockheed Martin-Boeing]] joint venture [[United Launch Alliance]]. The rocket consists of a first stage powered by kerosene and liquid oxygen, which uses a Russian made RD-180 engine, and a liquid hydrogen–liquid oxygen powered [[Centaur]] upper stage.
+
The '''Atlas V''' rocket is an expendable launch vehicle built by the [[Lockheed Martin]]-[[Boeing]] joint venture [[United Launch Alliance]]. The rocket consists of a first stage powered by kerosene and liquid oxygen, which uses a Russian made RD-180 engine, and a liquid hydrogen–liquid oxygen powered [[Centaur]] upper stage crafted by the American rocket manufacturer [[w:Aerojet_Rocketdyne|Aerojet Rocketdyne]].
  
The Atlas V rocket was used to launch the [[Mars Reconnaissance Orbiter]] on August 12, 2005.
+
The Atlas V rocket was used to launch the [[Mars Reconnaissance Orbiter]] on August 12, 2005, as well as the Mars Science Laboratory, the MAVEN Mars Orbiter, the InSight Mars and the Mars 2020-Perseverance mission.
 +
 
 +
Atlas V has a capacity to LEO of 8000 to 18500 kg.
 +
 
 +
Launch systems list.
 
   
 
   
[[category:Launch vehicles]]
+
{{stub}}
 +
[[category:Exploration Transport Systems]]
 +
[[category:Astronautics]]

Latest revision as of 06:16, 6 October 2021

The Atlas V Rocket launches the Mars Reconnaissance Orbiter into space.

The Atlas V rocket is an expendable launch vehicle built by the Lockheed Martin-Boeing joint venture United Launch Alliance. The rocket consists of a first stage powered by kerosene and liquid oxygen, which uses a Russian made RD-180 engine, and a liquid hydrogen–liquid oxygen powered Centaur upper stage crafted by the American rocket manufacturer Aerojet Rocketdyne.

The Atlas V rocket was used to launch the Mars Reconnaissance Orbiter on August 12, 2005, as well as the Mars Science Laboratory, the MAVEN Mars Orbiter, the InSight Mars and the Mars 2020-Perseverance mission.

Atlas V has a capacity to LEO of 8000 to 18500 kg.

Launch systems list.

This article is a stub. You can help Marspedia by expanding it.